Skip to main content
Advertisement
Browse Subject Areas
?

Click through the PLOS taxonomy to find articles in your field.

For more information about PLOS Subject Areas, click here.

< Back to Article

Table 1.

Context of use.

More »

Table 1 Expand

Fig 1.

a) Schematic of the FDA nozzle model b) Cross-sectional cuts identify validation locations along the nozzle axis c) An image of the three grids (inside the red oval region) used for the grid convergence study (snapshot taken at the sudden expansion location).

More »

Fig 1 Expand

Table 2.

Values of the input parameters used for the input parameter uncertainty analysis.

More »

Table 2 Expand

Table 3.

Details of the grids used for the grid convergence study.

More »

Table 3 Expand

Fig 2.

Qualitative explanation of the threshold approach for two different scenarios Black—Threshold; Green—CFD simulation and Blue—Experiment.

[] represent mean±uncertainty. a) Model is valid and b) Model not necessarily valid. In scenario (a), both the experiments and simulations are far away from the threshold and CIE smaller than CIΩ. In scenario (b), the simulations are closer to the threshold than to the experiments and CIE is larger than CIΩ.

More »

Fig 2 Expand

Fig 3.

Velocity vs axial and radial distances with uncertainty bars for both CFD and PIV for Re = 3500.

More »

Fig 3 Expand

Fig 4.

Velocity vs axial and radial distances with uncertainty bars for both CFD and PIV for Re = 6500.

More »

Fig 4 Expand

Fig 5.

Shear stress vs radial distance with uncertainty bars for both CFD and PIV.

More »

Fig 5 Expand

Fig 6.

p-value vs radial distance at three axial locations i) entrance, z = 0.088m, ii) throat, z = -0.02 m, and iii) throat, z = -0.008 m.

For reference, a straight line depicting p = 0.05 is shown in the figure. The p-values where obtained after performing a student’s t-test comparing the CFD and PIV shear stress datasets.

More »

Fig 6 Expand

Fig 7.

Confidence interval for |threshold-S| represented as CIΩ and Error, E expressed as CIE for a) entrance b) and c) throat for Re = 3500.

Two lines for each CI represent the upper and lower bound values.

More »

Fig 7 Expand

Fig 8.

Confidence interval for |threshold-S| represented as CIΩ and Error, E expressed as CIE for a) entrance b) and c) throat for Re = 6500.

Two lines for each CI represent the upper and lower bound values.

More »

Fig 8 Expand

Fig 9.

p-value vs radial distance at three axial locations i) z = 0.088m, ii) z = -0.02 m, and iii) z = -0.008 m for a) Re = 3500 and b) Re = 6500.

For reference, a straight line depicting p = 0.05 is shown in the figure. The p-values where obtained after performing a Student’s t-test for Ω = |threshold—S| and E = |S-D|.

More »

Fig 9 Expand

Fig 10.

Sensitivity of center-line velocity (a) and Comparison error, E (b) to the choice of the turbulence model.

More »

Fig 10 Expand

Fig 11.

a) Centerline velocity vs axial distance at Re = 2000, b) Confidence interval for |threshold-S| represented as CIΩ and Error, E expressed as CIE at the throat for Re = 2000.

Two lines for each CI represent the upper and lower bound values.

More »

Fig 11 Expand